FR3012245B1 - METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT - Google Patents

METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT Download PDF

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Publication number
FR3012245B1
FR3012245B1 FR1302433A FR1302433A FR3012245B1 FR 3012245 B1 FR3012245 B1 FR 3012245B1 FR 1302433 A FR1302433 A FR 1302433A FR 1302433 A FR1302433 A FR 1302433A FR 3012245 B1 FR3012245 B1 FR 3012245B1
Authority
FR
France
Prior art keywords
aircraft
arrival
ind
flight
estimated
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1302433A
Other languages
French (fr)
Other versions
FR3012245A1 (en
Inventor
Jerome Sacle
Herve Goutelard
Patrick Delpy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thales SA
Original Assignee
Thales SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales SA filed Critical Thales SA
Priority to FR1302433A priority Critical patent/FR3012245B1/en
Priority to US14/517,458 priority patent/US20150302671A1/en
Publication of FR3012245A1 publication Critical patent/FR3012245A1/en
Application granted granted Critical
Publication of FR3012245B1 publication Critical patent/FR3012245B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0816—Indicating performance data, e.g. occurrence of a malfunction
    • G07C5/0825—Indicating performance data, e.g. occurrence of a malfunction using optical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0095—Aspects of air-traffic control not provided for in the other subgroups of this main group
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06Q—INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES; SYSTEMS OR METHODS SPECIALLY ADAPTED FOR ADMINISTRATIVE, COMMERCIAL, FINANCIAL, MANAGERIAL OR SUPERVISORY PURPOSES, NOT OTHERWISE PROVIDED FOR
    • G06Q10/00—Administration; Management
    • G06Q10/04—Forecasting or optimisation specially adapted for administrative or management purposes, e.g. linear programming or "cutting stock problem"
    • G06Q10/047—Optimisation of routes or paths, e.g. travelling salesman problem

Abstract

Ce procédé de détermination d'une pluralité d'indicateurs de performance (Ind ) relatifs au vol d'un aéronef à destination d'un lieu d'arrivée est mis en œuvre par un dispositif électronique, l'aéronef comprenant une mémoire apte à stocker un plan de vol de l'aéronef et une valeur prédéterminée d'une quantité prévue de carburant consommé pendant le vol, le plan de vol comportant un instant prévu d'arrivée au lieu d'arrivée. Le procédé comprend le calcul (110) d'un premier indicateur de performance (Ind ) en fonction d'un instant estimé d'arrivée de l'aéronef au lieu d'arrivée, d'un temps estimé de vol de l'aéronef depuis son décollage jusqu'à son arrivée au lieu d'arrivée, et d'une quantité estimée de carburant consommé par l'aéronef jusqu'au lieu d'arrivée. Le procédé comprend en outre le calcul (120, 130) d'au moins un autre indicateur de performance parmi des deuxième (Ind ) et troisième (Ind ) indicateurs de performance, le deuxième indicateur de performance (Ind ) étant calculé en fonction d'un écart temporel entre l'instant d'arrivée estimé et l'instant d'arrivée prévu, et le troisième indicateur de performance (Ind ) étant calculé en fonction d'un écart de consommation entre la quantité de carburant consommé estimée et la quantité de carburant consommé prévue et d'au moins une grandeur supplémentaire parmi le groupe consistant en : un niveau du bruit généré par l'aéronef et une durée d'utilisation d'un moteur électrique auxiliaire alimenté par des turbines de l'aéronef.This method of determining a plurality of performance indicators (Ind) relating to the flight of an aircraft to a destination is implemented by an electronic device, the aircraft comprising a memory capable of storing a flight plan of the aircraft and a predetermined value of an anticipated amount of fuel consumed during the flight, the flight plan including an expected time of arrival at the destination. The method comprises calculating (110) a first performance indicator (Ind) based on an estimated time of arrival of the aircraft at the destination, an estimated flight time of the aircraft from takeoff until arrival at the place of arrival, and an estimated amount of fuel consumed by the aircraft to the place of arrival. The method further comprises calculating (120, 130) at least one other performance indicator from second (Ind) and third (Ind) performance indicators, the second performance indicator (Ind) being calculated based on a time difference between the estimated arrival time and the expected arrival time, and the third performance indicator (Ind) being calculated according to a difference in consumption between the estimated fuel consumption quantity and the quantity of fuel consumed. expected fuel consumption and at least one additional quantity from the group consisting of: a noise level generated by the aircraft and a duration of use of an auxiliary electric motor powered by turbines of the aircraft.

FR1302433A 2013-10-21 2013-10-21 METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT Active FR3012245B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1302433A FR3012245B1 (en) 2013-10-21 2013-10-21 METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT
US14/517,458 US20150302671A1 (en) 2013-10-21 2014-10-17 Method and device for determining a plurality of performance indicators relating to the flight of an aircraft, and associated computer program product

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1302433 2013-10-21
FR1302433A FR3012245B1 (en) 2013-10-21 2013-10-21 METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT

Publications (2)

Publication Number Publication Date
FR3012245A1 FR3012245A1 (en) 2015-04-24
FR3012245B1 true FR3012245B1 (en) 2019-05-24

Family

ID=49989835

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1302433A Active FR3012245B1 (en) 2013-10-21 2013-10-21 METHOD AND DEVICE FOR DETERMINING A PLURALITY OF PERFORMANCE INDICATORS RELATING TO THE FLIGHT OF AN AIRCRAFT, AND ASSOCIATED COMPUTER PROGRAM PRODUCT

Country Status (2)

Country Link
US (1) US20150302671A1 (en)
FR (1) FR3012245B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10640230B2 (en) * 2018-04-04 2020-05-05 Jurgen R. Ihns Cockpit pressurization and oxygen warning system
FR3099962B1 (en) * 2019-08-16 2022-09-09 Airbus Operations Sas System and method for predicting the time of occupation of a runway by an aircraft

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030093219A1 (en) * 2001-09-20 2003-05-15 Honeywell Inc. Four-dimensional route planner
US7228207B2 (en) * 2002-02-28 2007-06-05 Sabre Inc. Methods and systems for routing mobile vehicles
FR2907541B1 (en) * 2006-10-24 2009-01-16 Thales Sa METHOD FOR AUTOMATICALLY MANAGING THE SPEED OF A TURBULENT AIR AIRCRAFT AND DEVICE FOR CARRYING OUT SAID METHOD
US7606658B2 (en) * 2007-09-12 2009-10-20 Honeywell International Inc. Financial decision aid for 4-D navigation

Also Published As

Publication number Publication date
FR3012245A1 (en) 2015-04-24
US20150302671A1 (en) 2015-10-22

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